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Information × Registration Number 0225U000787, (0124U003067) , R & D reports Title Ensuring the development of the scientific direction "Technical Sciences" National Technical University "Kharkiv Polytechnic Institute" for 2024 popup.stage_title Забезпечення розвитку наукового напряму "Технічні науки" Національного технічного університету "Харківський політехнічний інститут" на 2024 рік Head Marchenko Andrii Р., Доктор технічних наук Registration Date 19-01-2025 Organization National Technical University "Kharkiv Polytechnic Institute" popup.description1 Implementation of the tasks of the long-term development plan of the National Technical University "Kharkiv Polytechnic Institute" in the scientific direction "Technical Sciences" for 2024 popup.description2  As a result of the work in the scientific direction "Technical Sciences" for 2024, the following results were obtained: 1. The type and parameters of acoustic antenna sensors, their number and location scheme were selected and justified. Criteria for evaluating the current sound (target sound of a shot) were developed for its preservation as an object of further analysis. 2. Software was developed for assessing the quality of the image stabilization system. 3. Requirements were created and draft design documentation was developed for the manufacture of an experimental model of a high-energy system. 4. The mathematical model of the hybrid MC was improved and adapted for the purposes of computer modeling. Simplified algorithms for automatic control of the hybrid MC were obtained. The architecture of a swarm of multicopters was developed, which assumes the presence of a MC leader and a rational distribution of information processing functions between the leader and swarm agents. 5. New theoretical and practical knowledge and data on the comprehensive improvement of the working process and engine design were obtained to ensure indicators and characteristics that meet the world level and ensure an increase in the level of specific power to 2.7 kW/kg of a two-stroke UAV engine, the power of which increases to 41 kW, and the specific effective fuel consumption decreases to 405 g/(kW h). 6. The characteristics of the multicomponent BaO-Al2O3-ZrO2-SiO2 system under study were determined, and the principles for selecting composition ranges suitable for the synthesis of radiation-resistant binders were substantiated. Product Description popup.authors Yeresko Oleksandr V. Volodymyr V. Ivakhno Avramenko Borys Andrіeіew Yuriі M. Akhiiezer Olena B. Bilyk Serhii Yu. Buriakovskyi Serhii H. Veretelnikov Mykola .. Haluza Oleksii A. Hamova Olha O. Dohadailo Oleksandr Zamaruiev Volodymyr V. Karpenko Nataliia Kovalov Artem V. Kravchenko Serhii S. Kryvosheiev Serhii Yu. Leshсhenko Viacheslav Mahula Andrii . Pitak Yaroslav M. Protsai Nataliia T. Sviezhentseva Olha Slipchenko Оlena V. Styslo Bohdan O. Subbotin Oleksandr V. Uspenskyi Valerii B. Shabanova Halyna M. Shyriaieva Nataliia Yu. Shumeiko Vita M. Shсhukina Liudmyla P. popup.nrat_date 2025-01-19 Close